Secure transmission of an aircraft trajectory

• US 9,786,184 B2
• Filed: 01/17/2014
• Issued: 10/10/2017
• Est. Priority Date: 02/13/2013
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: La Civita, Marco, Vilaplana, Miguel, Pena Ortiz, Nicolas
• Primary Examiner(s): Ismail, Mahmoud
• Application Number:
  US14/157,618
• Publication Number:
  US 20140229094A1
• Time in Patent Office: 1,362 Days
• Field of Search: 701120
• CPC Class Codes: G08G 5/0004 Transmission of traffic-related information to or from an aircraft airborne radio transmission systems in general H04B7/185; airborne wireless networks H04W84/06
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

The present disclosure relates to the secure transmission of an aircraft trajectory that is to be flown or that has been flown. A ground-referenced description of the trajectory of the aircraft expressed in ground-referenced parameters is converted, using a description of an imaginary atmospheric model describing imaginary atmospheric conditions along the trajectory, into an air-referenced description of the aircraft trajectory expressed in air-referenced parameters. For decryption, knowledge of the imaginary atmospheric conditions allows the air-referenced description of the aircraft trajectory to be converted back into the ground-referenced description of the aircraft trajectory. Thus, the ground-referenced trajectory may be though of as the plain text, the imaginary atmospheric model as the cipher key and the air-referenced trajectory as the cipher text.

Claims

1. A computer-implemented method of communicating an aircraft trajectory using encryption and decryption of a description of the aircraft trajectory, comprising:

on a sender'"'"'s side;

obtaining a ground-referenced description of the trajectory of the aircraft expressed in ground-referenced parameters;

obtaining a description of a fictional atmospheric model describing fictional atmospheric conditions along the trajectory;

using the description of the fictional atmospheric model to encrypt the ground-referenced description of the aircraft trajectory by converting the ground-referenced description of the aircraft trajectory into an air-referenced description of the aircraft trajectory expressed in air-referenced parameters with respect to the fictional atmospheric model; and

making available to the receiver the description of the fictional atmospheric conditions and air-referenced data from which the aircraft trajectory is unambiguously determined;

and

on a receiver'"'"'s side;

receiving the description of the fictional atmospheric conditions and the air-referenced data from which the aircraft trajectory is unambiguously determined;

using the description of the fictional atmospheric conditions to decrypt air-referenced data from which the aircraft trajectory is unambiguously determined by converting the air-referenced data from which the aircraft trajectory is unambiguously determined back into the ground-referenced description of the aircraft trajectory expressed in ground-referenced parameters;

obtaining a description of a real atmospheric model describing real atmospheric conditions along the trajectory;

obtaining an aircraft performance model that describes how the aircraft performs; and

using the description of a real atmospheric model and an aircraft performance model to convert the ground-referenced description of the aircraft trajectory into a description of aircraft intent corresponding to a computer language description expressed using a formal language, wherein the description of the aircraft intent is a description of how the aircraft is to be flown expressed as instructions that provides a complete description of the aircraft'"'"'s behavior such that all degrees of freedom of motion are defined, and using the description of aircraft intent to fly the aircraft.

2. The method of claim 1, wherein:

the air-referenced data from which the aircraft trajectory is unambiguously determined comprises air-referenced aircraft intent data that provides a description of aircraft intent of the aircraft expressed in air-referenced parameters corresponding to a computer language description expressed using a formal language, wherein the description of the aircraft intent is a description of how the aircraft is to be flown expressed as instructions that provides a complete description of the aircraft'"'"'s behavior such that all degrees of freedom of motion are defined and such that a unique trajectory is calculated unambiguously from the description of aircraft intent;

and the method comprises using the air-referenced description of the aircraft trajectory, the description of the fictional atmospheric model and an aircraft performance model that describes how the aircraft performs to generate the air-referenced aircraft intent data.

3. The method of claim 1, wherein the air-referenced data from which the aircraft trajectory is unambiguously determined is the air-referenced description of the aircraft trajectory expressed in air-referenced parameters with respect to the fictional atmospheric model.

4. The method of claim 1, wherein the ground-referenced description of the aircraft trajectory and/or the air-referenced description of the aircraft trajectory comprises one or more computer data files representing a time-evolving series of either ground-referenced or air-referenced parameters respectively.

5. The method of claim 4, wherein the ground-referenced parameters of the ground-referenced description of the aircraft trajectory comprise any of longitude, latitude, altitude, ground speed, bearing and direction.

6. The method of claim 4, wherein the air-referenced parameters of the air-referenced description of the aircraft trajectory comprise any of air speed, Mach, aerodynamic bearing, and aerodynamic flight path angle.

7. The method of claim 1, further comprising, on the sender side:

obtaining a description of aircraft intent of the aircraft corresponding to a computer language description expressed using a formal language, wherein the description of the aircraft intent is a description of how the aircraft is to be flown expressed as instructions that provides a complete description of the aircraft'"'"'s behaviour such that all degrees of freedom of motion are defined and such that a unique trajectory is calculated unambiguously from the description of aircraft intent;

obtaining a description of a real atmospheric model describing real atmospheric conditions along the trajectory;

obtaining an aircraft performance model that describes how the aircraft performs; and

using the aircraft performance model and the description of the real atmospheric conditions to generate the ground-referenced description of the aircraft trajectory expressed in the ground-referenced parameters from the description of the aircraft intent.

8. The method of claim 1, wherein the method either:

comprises generating randomly the fictional atmospheric conditions;

or comprises obtaining a description of a real atmospheric model describing real atmospheric conditions along the trajectory and altering the real atmospheric conditions to form the fictional atmospheric conditions.

9. The method of claim 1, wherein the description of the fictional atmospheric conditions and the air-referenced data from which the aircraft trajectory is unambiguously determined are passed from sender to receiver separately.

10. The method of claim 1, comprising including in the air-referenced data from which the aircraft trajectory is unambiguously determined, a ground-referenced position of the aircraft, optionally a ground-referenced initial position of the aircraft.

11. A computer infrastructure operable to communicate an aircraft trajectory using encryption and decryption of a description of the aircraft trajectory, comprising an encryption computer system and a decryption computer system, wherein

the encryption computer system comprises:

memory operable to store a ground-referenced description of the trajectory of the aircraft expressed in ground-referenced parameters;

memory operable to store a description of a fictional atmospheric model describing fictional atmospheric conditions along the trajectory;

an encryption processor programmed to use the description of the fictional atmospheric model to encrypt the ground-referenced description of the aircraft trajectory by converting the ground-referenced description of the aircraft trajectory into an air-referenced description of the aircraft trajectory expressed in air-referenced parameters with respect to the fictional atmospheric model, and to make available to the decryption computer system the description of the fictional atmospheric conditions and air-referenced data from which the aircraft trajectory is unambiguously determined;

and

the decryption computer system comprises;

a receiver operable to receive the description of the fictional atmospheric conditions and the air-referenced data from which the aircraft trajectory is unambiguously determined;

memory operable to store the description of the fictional atmospheric conditions and the air-referenced data from which the aircraft trajectory is unambiguously determined;

a decryption processor programmed to;

use the description of the fictional atmospheric conditions to decrypt the air-referenced data from which the aircraft trajectory is unambiguously determined by converting the air-referenced data from which the aircraft trajectory is unambiguously determined back into the ground-referenced description of the aircraft trajectory expressed in ground-referenced parameters;

obtain a description of a real atmospheric model describing real atmospheric conditions along the trajectory;

obtain an aircraft performance model that describes how the aircraft performs; and

using the description of a real atmospheric model and an aircraft performance model to convert the ground-referenced description of the aircraft trajectory into a description of aircraft intent corresponding to a computer language description expressed using a formal language, wherein the description of the aircraft intent is a description of how the aircraft is to be flown expressed as instructions that provides a complete description of the aircraft'"'"'s behavior such that all degrees of freedom of motion are defined, and using the description of aircraft intent to fly the aircraft.

12. The computer infrastructure of claim 11, wherein:

the air-referenced data from which the aircraft trajectory is unambiguously determined comprises air-referenced aircraft intent data that provides a description of aircraft intent of the aircraft expressed in air-referenced parameters corresponding to a computer language description expressed using a formal language, wherein the description of the aircraft intent is a description of how the aircraft is to be flown expressed as instructions that provides a complete description of the aircraft'"'"'s behavior such that all degrees of freedom of motion are defined and such that a unique trajectory is calculated unambiguously from the description of aircraft intent; and

the encryption processor is further programmed to use the air-referenced description of the aircraft trajectory, the description of the fictional atmospheric model and an aircraft performance model that describes how the aircraft performs to generate the air-referenced aircraft intent data.

13. The computer infrastructure of claim 11, wherein the air-referenced data from which the aircraft trajectory is unambiguously determined is the air-referenced description of the aircraft trajectory expressed in air-referenced parameters with respect to the fictional atmospheric model.

14. The computer infrastructure of claim 11, wherein the ground-referenced description of the aircraft trajectory and/or the air-referenced description of the aircraft trajectory comprises one or more computer data files representing a time-evolving series of either ground-referenced or air-referenced parameters respectively.

15. The computer infrastructure of claim 14, wherein the ground-referenced parameters of the ground-referenced description of the aircraft trajectory comprise any of longitude, latitude, altitude, ground speed, bearing and direction.

16. The computer infrastructure of claim 11, wherein the description of the fictional atmospheric conditions and the air-referenced data from which the aircraft trajectory is unambiguously determined is made available from the encryption computer system to the decryption computer system separately.